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Viewing 1 to 30 of 5274
2016-08-29
Standard
AS264F
The desired system for aircraft instrument panel and cockpit lighting is one that will furnishlight of adequate intensity and distribution under all conditions of external lighting so that the crew may read instrumentation, placards, check lists, manuals, maps, instrument color coding, distinguish controls, etc., without undue interference with their vision outside of the aircraft.
2016-08-29
Standard
AIR1168/4B
This section presents the basic equations for computing ice protection requirements for nontransparent and transparent surfaces and for fog and frost protection of windshields. Simplified graphical presentations suitable for preliminary design and a description of various types of ice, fog, frost, and rain protection systems are also presented.
2016-08-17
WIP Standard
ARP4553B
This SAE Aerospace Recommended Practice (ARP) is intended to provide design and qualification requirements for self-displacing hydraulic accumulators.

These requirements are intended to be included in the Producrement Specification for the accumulator. Those requirements identified by the use of "shall" are considered to be essential requirements; those requirements identified by the use of "should" are considered to be optional requirements for inclusion in the Specificaiton at the discretion of the Purchaser.

In addition, test methods for production acceptance and qualification purposes are provided.

The accumulator is intended for use in military aerospace hydraulic systems with rated pressures of up to 8000 psi (55,158 kPa) and of the following types as specified in SAE AS 5440: Type I: -65 to +160 °F (-54 to +71 °C) fluid temperature; Type II: -65 to +275 °F (-54 to +135 °C) fluid temperature.

2016-08-16
WIP Standard
AS85049/138B
Scope unavailable.
2016-08-16
WIP Standard
AS4211E
Remove AS85421 performance specification and leave AS85720 performance specification to provide clarification regarding the QPL and associated pressure applications.
2016-08-16
WIP Standard
AS4220D
Remove AS85421 performance specification and leave AS85720 performance specification to provide clarification regarding the QPL and associated pressure applications.
2016-08-16
WIP Standard
AS4210E
Remove AS85421 performance specification and leave AS85720 performance specification to provide clarification regarding the QPL and associated pressure applications.
2016-08-16
WIP Standard
AS4224D
Remove AS85421 performance specification and leave AS85720 performance specification to provide clarification regarding the QPL and associated pressure applications.
2016-08-16
WIP Standard
AS4807D
Remove AS85421 performance specification and leave AS85720 performance specification to provide clarification regarding the QPL and associated pressure applications. Correct the “V” dimension for size 10.
2016-08-16
WIP Standard
AS4221D
Remove AS85421 performance specification and leave AS85720 performance specification to provide clarification regarding the QPL and associated pressure applications.
2016-08-16
WIP Standard
AS5002D
Remove AS85421 performance specification and leave AS85720 performance specification to provide clarification regarding the QPL and associated pressure applications..
2016-08-16
WIP Standard
AS5003D
Remove AS85421 performance specification and leave AS85720 performance specification to provide clarification regarding the QPL and associated pressure applications.
2016-08-16
WIP Standard
AS4809D
Remove AS85421 performance specification and leave AS85720 performance specification to provide clarification regarding the QPL and associated pressure applications.
2016-08-16
WIP Standard
AS5004D
Remove AS85421 performance specification and leave AS85720 performance specification to provide clarification regarding the QPL and associated pressure applications.
2016-08-12
Standard
AIR1184B
This report is intended to identify the various errors typically encountered in capacitance fuel quantity measurement systems. In addition to identification of error sources, it describes the basic factors which cause the errors. When coupled with appraisals of the relative costs of minimizing the errors, this knowledge will furnish a tool with which to optimize gauging system accuracy, and thus, to obtain the optimum overall system within the constraints imposed by both design and budgetary considerations. Since the subject of fuel measurement accuracy using capacitance based sensing is quite complex, no attempt is made herein to present a fully-comprehensive evaluation of all factors affecting gauging system accuracy. Rather, the major contributors to gauging system inaccuracy are discussed and emphasis is given to simplicity and clarity, somewhat at the expense of completeness. An overview of capacitive fuel gauging operation can be found in AIR5691.
2016-08-12
Standard
ARP741C
This paper describes a recommended practice and procedure for the correlation of test cells that are used for the performance testing of turbofan and turbojet engines. Test cell correlation is performed to determine the effect of any given test cell enclosure and equipment on the performance of an engine relative to the baseline performance of that engine. When baseline testing is performed in an indoor test cell, the baseline performance data are adjusted to open air conditions. Although no original equipment manufacturer (OEM) documents are actually referenced, the experience and knowledge of several OEMs contributed to the development of this document. Each engine Manufacturer has their own practices relating to correlation and they will be used by those OEMS for the purpose of establishing certified test facilities.
2016-08-10
WIP Standard
AIR6211A
This test method provides stakeholders (runway deicing chemical manufacturers, deicing/anti-icing chemical operators and airport authorities) with a relative ice penetration capacity of runway deicing/anti-icing chemicals, by measuring the ice penetration as a function of time. Such runway deicing/anti-icing chemicals are often also used on taxiways and other paved areas. This test method does not quantitatively measure the theoretical or extended time of ice penetration capability of ready-to-use runway deicing/anti-icing chemicals in liquid or solid form.
2016-08-10
WIP Standard
AIR6170A
This test method provides stakeholders (runway deicing chemical manufacturers, deicing/anti-icing chemical operators and airport authorities) with relative ice melting capacity of runway deicing chemicals, by measuring the amount of ice melted as a function of time. Such runway deicing chemicals are often also used on taxiways. This test method does not quantitatively measure the theoretical or extended time ice melting capability of ready-to-use runway deicing/anti-icing chemicals in liquid or solid form.
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